The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 22, 2021

Filed:

Feb. 05, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Gary E. Georgeson, Tacoma, WA (US);

Barry A. Fetzer, Renton, WA (US);

James J. Troy, Issaquah, WA (US);

Scott W. Lea, Renton, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01N 29/265 (2006.01); H04B 7/26 (2006.01); G01N 29/06 (2006.01); G01N 29/44 (2006.01); B64F 5/60 (2017.01); H04L 12/24 (2006.01); H04L 12/26 (2006.01); H04W 40/24 (2009.01); H04W 72/04 (2009.01); H04W 48/16 (2009.01); H04W 72/02 (2009.01);
U.S. Cl.
CPC ...
H04B 7/2656 (2013.01); B64F 5/60 (2017.01); G01N 29/0654 (2013.01); G01N 29/265 (2013.01); G01N 29/44 (2013.01); H04L 41/0695 (2013.01); H04L 43/16 (2013.01); H04W 40/244 (2013.01); H04W 72/0446 (2013.01); G01N 2291/0231 (2013.01); G01N 2291/0258 (2013.01); G01N 2291/0289 (2013.01); G01N 2291/2634 (2013.01); G01N 2291/2694 (2013.01); H04W 48/16 (2013.01); H04W 72/02 (2013.01); H04W 72/042 (2013.01); Y02D 30/70 (2020.08);
Abstract

Systems and methods for high-speed non-destructive inspection of a half- or full-barrel-shaped workpiece, such as a barrel-shaped section of an aircraft fuselage. Such workpieces can be scanned externally using a mobile (e.g., translating) arch gantry system comprising a translatable arch frame disposed outside the fuselage section, a carriage that can travel along a curved track carried by the arch frame, a radially inward-extending telescopic arm having a proximal end fixedly coupled to the carriage, and an NDI sensor unit coupled to a distal end of the telescoping arm. The stiffeners of the fuselage sections can be scanned using a mobile scanner platform disposed inside the fuselage section, which platform comprises a radially outward-extending telescopic arm rotatably coupled to a mobile (e.g., holonomic or linear motion) platform and an NDI sensor unit coupled to a distal end of the telescoping arm. The scan data is matched with position data acquired using any one of a plurality of tracking systems to enable the display of NDI features/flaws on a three-dimensional representation of the workpiece.


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